EP1154893A1 - Formkörper - Google Patents
FormkörperInfo
- Publication number
- EP1154893A1 EP1154893A1 EP00901601A EP00901601A EP1154893A1 EP 1154893 A1 EP1154893 A1 EP 1154893A1 EP 00901601 A EP00901601 A EP 00901601A EP 00901601 A EP00901601 A EP 00901601A EP 1154893 A1 EP1154893 A1 EP 1154893A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- staple fibers
- shaped body
- matrix
- fibers
- thermoplastic
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/22—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least two directions forming a two dimensional structure
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
- B29C70/465—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating by melting a solid material, e.g. sheets, powders of fibres
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
- B29B15/105—Coating or impregnating independently of the moulding or shaping step of reinforcement of definite length with a matrix in solid form, e.g. powder, fibre or sheet form
Definitions
- the present invention relates to fiber-reinforced molded articles formed from a textile fabric, means and a method for their production and their use 5
- thermoplastic molding compound and glass fiber mats are processed in a pressing process to form a fiber composite material.
- This process is predominantly suitable for the production of sheet-like semi-finished products. It is disadvantageous that essentially only flat-shaped structures or sheet-like structures can be produced Components cannot be manufactured or can only be manufactured indirectly in an additional forming step using the flat sheet-metal structures
- the object of the present invention is to avoid these disadvantages and in particular to create 15 shaped bodies and a method for their production which, starting from a fiber material, lead to shaped bodies or components in one operation and in short processing times
- the molded body contains a mat ⁇ x, which is the re-solidified product of 20 staple fibers made of at least one thermoplastic first material that has been brought into a plastic state, and embedded in the mat ⁇ x, staple fibers made of at least a second material, the softening, melting or decomposition point of the staple fibers from the second material lies above the softening or melting point of the first material and the fiber orientation of the second material in the material corresponds to the fiber orientation of the textile fabric
- the textile flat structures can be sewn fibers in redirectional layers, in bidirectional layers, as cut rovings, scrims, woven or knitted fabrics
- the staple fibers of the first material expediently have an average length of 10 to 150 mm, expediently 30 to 120 mm, preferably 60 to 100 mm and in particular 75 to 85 mm
- the staple fibers of the second material expediently have an average length of 10 to 35 150 mm, expediently 30 to 120 mm, preferably 60 to 100 mm and in particular 75 to 85 mm
- the textile fabrics contain staple fibers made of the first and the second material, each with an average length of 75 to 85 mm.
- the staple fibers made of the first thermoplastic material can contain or consist of, for example, polyamides, polyesters, polycarbonates, polyurethanes, polyureas, polyolefins, polystyrenes, polyacrylonitriles, polyvinyl chloride, polyvinylidene chloride, polyvinyl alcohol or polytetrafluoroethylene.
- the staple fibers from the second material are e.g. high temperature resistant inorganic or organic fibers.
- organic staple fibers can be fully aromatic polyamides, aramids, aromatic polyamides containing heterocycles, polyimides, polyimidamides, polybenzimidazoles, polyoxdiazoles, polytriazoles, polythiadiazoles, polybenzoxazoles, polyquinazolidines, poly-bis-benzimidazolbenzophenanthralamide or choline-containing azalethazalines or choline-azimethalonazoles.
- inorganic staple fibers which expediently contain or consist of glass, slag, stone, ceramic, quartz, silica glass, boron, silicon carbide, boron nitride, boron carbide, aluminum oxide, zirconium oxide, steel, aluminum, tungsten, carbon or graphite, or it can be single-crystalline corundum or be single crystalline silicon carbide. Staple fibers made of glass, carbon or graphite are preferred.
- staple fibers made of natural materials which suitably contain or consist of cotton, wool, silk, or fibers made of jute, sisal, coconut, linen or hemp etc.
- the staple fibers made of thermoplastic material and in particular the staple fibers made of organic materials made of the second material, can contain fire-retardant additives, pigments, dyes, fillers, etc.
- the temperature range of the softening, melting or decomposition point of the staple fibers made of the second material is, for example, chosen such that it is at least 5%, expediently 10% and in particular 30% above the softening or melting point of the first material.
- the staple fibers made of the second material are in the matrix as directional fibers in unidirectional layers, in bidirectional layers, as cut rovings, scrims, woven or knitted fabrics, which form the re-solidified product from staple fibers made from a plastic state thermoplastic first material is embedded.
- the fiber orientation of the original textile remains The fabric of the staple fibers of the second material is advantageously obtained.
- the staple fiber can be stretched from the second material, for example in a fiber sliding process, under an externally applied forming force. The stretching of the staple fiber and the second material in particular takes place from its thickness, that is to say with a decrease in thickness.
- the softened or melted thermoplastic first material can bring about a fiber sliding effect between the individual fibers or fibrils of the second material.
- the staple fibers made of the second material can be stretched by up to 20%, expediently by up to 35% and preferably by up to 50% of their original length in the textile fabric.
- the textile fabrics made of directional fibers in unidirectional layers, in bidirectional layers, the cut rovings, scrims, woven or knitted fabrics can be in one or more layers, for example 1-, 2-, 3-, 4-, 5- etc. layers are used, according to the desired final thickness and strength of the molded body.
- the stretching of, for example, up to 20% can advantageously be achieved in the case of 1-layer textile fabrics, while the stretching of up to 35% and higher can advantageously be carried out with multi-layer, for example 4-layer, textile fabrics.
- the textile fabrics can have, for example, a density of 100 to 1000 g / m 2 .
- the staple fibers made of the second material relate to 40 to 70%, suitably 50 to 60% and preferably 53 to 59%, and accordingly the matrix made of the thermoplastic first material relates to 60, based on the volume up to 30%, suitably 50 to 40% and preferably 47 to 41%.
- the present invention also includes textile fabrics made of directional fibers in unidirectional layers, bidirectional layers, as cut rovings, scrims, woven or knitted fabrics made from a mixture of staple fibers from at least two materials, the staple fibers made from at least one thermoplastic first material in proportions of 60 up to 30%, based on the volume, and the staple fibers made of at least one second material are present in proportions of 40 to 70%, based on the volume, for the production of the shaped bodies according to the invention.
- the staple fibers are made of a hybrid yarn or a mixed yarn made of the first material or the first materials and the second material or the second materials.
- the hybrid yarn from the staple fibers is processed into a woven fabric, for example.
- the fabric can be a 1 - 1, 1 - 2, 1 - 3, 1 - 4, 1 - 5, etc. fabric. Ie the weft threads can alternately under or 1, 2, 3, 4, 5, etc. warp threads. spread.
- the fiber orientation can be, for example, 0 90 °.
- a 4 l satin fabric is particularly preferred.
- the textile fabrics can be used in 1, 2, 3, 4, 5, etc. layers, with 1, 2, 3, 4 or 5-layer fabrics being preferred.
- a higher number of layers can also be used, or the number of layers within a shaped body can vary. For example, heavily used areas on the finished molded part can be made stronger by a multiplicity of layers, while less used areas are constructed by one or a few layers.
- the fiber orientation of the individual layers can be the same or twisted and / or offset.
- the oriented fibers in unidirectional layers, bidirectional layers, as cut rovings, scrims, fabrics or knitted fabrics, and in particular the staple fibers made of the second material can coat plastic on their surface with adhesion promoters such as adhesive-containing coatings, such as PA 6.6 coatings, etc., be equipped.
- the directional fibers in unidirectional layers, bidirectional layers, as cut rovings, scrims, fabrics or knitted fabrics made from a mixture of staple fibers from at least two materials can be subjected to a drying process before shaping, the drying at elevated temperature, for example at temperatures in one area from 60 to 110 ° C, and / or in a vacuum, for example at 100 to 500 mbar.
- the moldings according to the invention formed from textile fabrics, can be produced by the textile fabric made from directional fibers in unidirectional layers, bidirectional layers, as cut rovings, scrims, woven or knitted fabrics made from a mixture of staple fibers from at least two materials, the staple fibers being made from white - Relate at least one thermoplastic first material to 60 to 30% by volume and preheat the staple fibers from at least one second material to 40 to 70% by volume, softening or melting the first material while forming the matrix and then deformed by means of a pressing process to the intended molded body.
- the pressing process takes place in a tool or die and under pressure by means of a stamp or patrix for shaping and at temperatures of the stamp and the tool below the softening or melting temperatures of the first material. This process is also called the cold stamping process.
- the preheating can be done by radiation, such as IR radiation, by convection, etc.
- the preheating temperature depends on the melting temperature of the first material and is above the melting point of the first material and below a softening, Melting or decomposition point of the second material.
- a preheating temperature of up to 250 ° C can be used.
- the textile fabric can, for example, be placed on a frame or heated in a frame stretched by radiation or can be heated by contact heating lying on a heat source. In the latter case, the first material must be prevented from sticking to the heated pad.
- the temperature of the textile fabric must be increased until it is plastically deformed or the first material melts.
- the preheated textile fabric with the softened or melted first material is plastically deformed, at least to the extent that its fiber structure disappears and a matrix is formed, while the staple fibers of the second material retain their fiber structure and fiber orientation - embedded in the matrix. Ie there is a consolidation.
- the preheated textile fabric is then fed to the next treatment step.
- the shape can be, for example, a tool, a die or a die.
- the staple fibers can be inserted or placed as a consolidated preheated textile fabric in the form of directional fibers in unidirectional layers, bidirectional layers, as cut rovings, scrims, woven or knitted fabrics from the mixture of staple fibers in the tool, also called a die or die, and by means of a rigid or elastic stamp, also called patrix, can be pressurized.
- the deformation can be carried out at an essentially constant temperature of the tool or of the tool and punch.
- the temperature of the tool or of the tool and punch is advantageously slightly below the softening or melting temperature of the first material.
- the matrix containing the staple fibers from the second material should be sufficient for the deformation step.
- the matrix and the staple fibers of the second material embedded therein are forced into the shape of the tool and the stamp to form the shaped body.
- a partial cooling takes place between the tool and the stamp, the matrix formed from the first material solidifying.
- the molded body can then already be removed from the tool.
- the cooling to ambient temperature can take place outside the mold.
- the dwell time in the press for the deformation can be, for example, less than 20 seconds, advantageously less than 10 seconds, and in particular 3 to 6 seconds.
- a typical dwell time is 5 seconds.
- the textile fabrics made of directional fibers in unidirectional layers, bidirectional layers, as cut rovings, scrims, fabrics or knitted fabrics deform according to the negative shape of the tool and the stamp.
- Isostatic pressing is preferred.
- Isostatic pressing is advantageously carried out by means of a rubber-elastic stamp. This can be used, for example, to form molded parts with a base part and sloping or vertical side walls, or undercuts can also be formed for multi-part tools.
- the deformation can be carried out according to the principle of deep drawing, that is to say the deformation while retracting the material with the material thickness remaining the same, stretching, that is to say by fixing the material along its side edges by means of a hold-down device and stretching the material with a decrease in thickness, a combination of stretching and deep drawing, that is to say partial retraction of the material to be shaped, or by vacuum forming.
- Stretch drawing is preferred.
- the staple fibers of the second material - taken up in the matrix formed from the first material - are subject to an elongation with a simultaneous decrease in thickness.
- the individual fibers or fibrils which form the staple fibers are essentially enveloped by the plastic or melted thermoplastic first material and, supported by a resulting fiber sliding effect, the elongation takes place in a fiber sliding process with a decrease in the thickness of the staple fiber.
- a drawing ratio ⁇ of 1 to 3, preferably of 1.2 to 2.1 and in particular of 1.8 to 2.0 can be used.
- the draw ratio ⁇ is the quotient of the stored length a to the extended length b.
- the stored length a corresponds to the actual wall length of the shaped body
- the stretched length b corresponds to the length of the projection of the shaped body.
- the tool or the die can be heated.
- At least the deformation-active surface can be made of chromium, chromium steel, nickel, Teflon, nickel-Teflon etc. for easy demolding.
- the metallic surfaces are expediently smooth and in particular polished or lapped. Release agents and / or non-stick agents can also be applied for easy demolding after the pressing process.
- At least the deformation-effective parts of a rubber-elastic male or a rubber-elastic stamp are made of silicone rubber, for example.
- the patrix or the stamp can also be heated.
- the temperature for the deformation of the consolidated material inserted between the tool and the punch depends on the softening or melting temperature of the first material.
- the temperature for deformation and consolidation is advantageously below the melting point and in particular below the crystallization temperature of the first material.
- temperatures from 70 ° C. to 160 ° C. are expedient, temperatures from 110 ° C. to 150 ° C. being advantageous.
- the pressures are, for example, 25 to 100 bar, expediently 40 to 60 bar and in particular 50 bar.
- the thickness of the moldings according to the invention can be selected in accordance with the thickness of the textile fabric and the number of layers pressed together. Typical thicknesses of moldings are, for example, from 0.5 to 5 mm.
- the thickness within a shaped body can be varied.
- the shaped bodies can be, for example, profile-like structural parts or sheet-like parts (so-called organic sheets), etc.
- the moldings according to the present invention can be used on vehicles for water, road or rail or on stationary buildings.
- Examples of such parts are doors, hoods, side parts, front and rear aprons, bumpers, panels, partitions, reinforcements or brackets on vehicle bodies; Panels, walls, partition walls, floors, ceilings or parts thereof, on buses or railway carriages, cladding, partition walls etc. in ships, cladding, partition walls, partition walls, floor or ceiling elements on exterior facades or in the interior of stationary buildings, such as buildings etc.
- Preferred applications are doors, hoods, side parts, front and rear aprons, bumper surfaces, floor groups and roofs or parts thereof for passenger cars and light commercial vehicles.
- a fiber mat with a basis weight of 500 g / cm 2 from 4 layers of a satin 4-1 fabric with a 0790 ° fiber orientation made from staple fiber hybrid yarn, essentially from 44 vol.% Polyamide staple fibers and 56 vol.% Carbon staple fibers with an average length of 80 mm are placed on a frame by IR radiation and heated to approx. 220 ° C. within 75 seconds and held at this temperature for approx. 10 seconds for consolidation.
- the polyamide staple fibers lose their structure and form a matrix that envelops the carbon fibers.
- This preheated intermediate product is placed on the tool heated to approx. 150 ° C, fixed on the edge with a hold-down device and the stamp with the rubber-elastic shaping surface in the Tool lowered.
- the closing time of the press is about 3 seconds, the pressure used is 50 bar and the dwell time under pressure in the press is 5 seconds.
- the intermediate product deforms plastically from the fiber mat.
- the desired contours of the molded body are formed from the matrix by the negative shape of the tool and by the stamp.
- the carbon fibers stretch, respectively. lengthen during the pressing process due to the fiber sliding effect with a decrease in thickness according to the depth of deformation of the tool.
- the negative shape of the tool offers a conical depression.
- the intermediate product from the fiber mat is pressed into the depression by the punch, the staple fibers of the second material depending on their position in the conical depression requiring up to 35% of their original length. The original fiber orientation of the fabric is retained.
- the finished molded body can be removed from the tool and occasionally by deburring and / or by other treatments, such as painting. Covering foils and the like can be further processed.
- the thickness of the molded body is approximately 1.5 mm.
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Reinforced Plastic Materials (AREA)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Nonwoven Fabrics (AREA)
Abstract
Description
Claims
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH00300/99A CH693627A5 (de) | 1999-02-17 | 1999-02-17 | Faserverstärkter Formkörper. |
CH30099 | 1999-02-17 | ||
PCT/EP2000/000648 WO2000048824A1 (de) | 1999-02-17 | 2000-01-28 | Formkörper |
Publications (2)
Publication Number | Publication Date |
---|---|
EP1154893A1 true EP1154893A1 (de) | 2001-11-21 |
EP1154893B1 EP1154893B1 (de) | 2003-09-03 |
Family
ID=4183861
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP00901601A Expired - Lifetime EP1154893B1 (de) | 1999-02-17 | 2000-01-28 | Formkörper |
Country Status (7)
Country | Link |
---|---|
EP (1) | EP1154893B1 (de) |
JP (1) | JP2002537146A (de) |
AU (1) | AU765119B2 (de) |
CA (1) | CA2368046A1 (de) |
CH (1) | CH693627A5 (de) |
DE (1) | DE50003528D1 (de) |
WO (1) | WO2000048824A1 (de) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU2005328677B2 (en) * | 2005-03-07 | 2011-03-10 | Spunfab, Ltd. | Thermoplastic nylon adhesive matrix having a uniform thickness and composite laminates formed therefrom |
EP1787790A1 (de) * | 2005-11-21 | 2007-05-23 | Lankhorst Indutech B.V. | Verfahren zur Verformung eines thermoplastischen Verbundwerkstoffes |
DE102010028433A1 (de) * | 2010-04-30 | 2011-11-03 | Deutsche Institute Für Textil- Und Faserforschung Denkendorf | Hybridgarn zur Herstellung von Formteilen |
WO2013177744A1 (zh) * | 2012-05-28 | 2013-12-05 | Cai Zilin | 改良家纺用布 |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6445841A (en) * | 1987-08-13 | 1989-02-20 | Nitto Boseki Co Ltd | Fabric for fiber reinforced thermoplastic resin laminate material |
CA2122548A1 (en) * | 1993-05-25 | 1994-11-26 | George M. Kent | Reinforcing composite items with composite thermoplastic staple fibers |
GB9620408D0 (en) * | 1996-09-01 | 1996-11-20 | New Millennium Composites Ltd | Manufacture of fibre reinforced composites |
-
1999
- 1999-02-17 CH CH00300/99A patent/CH693627A5/de not_active IP Right Cessation
-
2000
- 2000-01-28 WO PCT/EP2000/000648 patent/WO2000048824A1/de active IP Right Grant
- 2000-01-28 AU AU22939/00A patent/AU765119B2/en not_active Ceased
- 2000-01-28 EP EP00901601A patent/EP1154893B1/de not_active Expired - Lifetime
- 2000-01-28 JP JP2000599587A patent/JP2002537146A/ja not_active Withdrawn
- 2000-01-28 CA CA002368046A patent/CA2368046A1/en not_active Abandoned
- 2000-01-28 DE DE50003528T patent/DE50003528D1/de not_active Expired - Fee Related
Non-Patent Citations (1)
Title |
---|
See references of WO0048824A1 * |
Also Published As
Publication number | Publication date |
---|---|
EP1154893B1 (de) | 2003-09-03 |
WO2000048824A1 (de) | 2000-08-24 |
CA2368046A1 (en) | 2000-08-24 |
AU2293900A (en) | 2000-09-04 |
DE50003528D1 (de) | 2003-10-09 |
CH693627A5 (de) | 2003-11-28 |
AU765119B2 (en) | 2003-09-11 |
JP2002537146A (ja) | 2002-11-05 |
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